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LT - STREAMLINE AIRFRAME WITH BOUNDARY INGESTION FLUIDIC PROPULSIVE ELEMENTS
EN - STREAMLINE AIRFRAME WITH BOUNDARY INGESTION FLUIDIC PROPULSIVE ELEMENTS

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Patent not validated

Bibliographic data
Indications of the International Patent Classification (IPC)
(51) INT.CL. B64C 21/06 (2023.01)
F02C 3/04 (2013.01)
B64C 23/00 (2006.01)
F02C 6/04 (2013.01)
B64C 39/12 (2006.01)
F02K 1/002 (2013.01)
F01N 13/10 (2010.01)
F02K 1/36 (2013.01)
F02C 6/08 (2006.01)
Y02T 50/10 (2013.01)
F02K 1/38 (2006.01)
B64C 21/06 (2013.01)
B64C 23/005 (2013.01)
European patent
(11) Number of the document 3802323
(13) Kind of document T
(96) European patent application number 19811198.1
Date of filing the European patent application 2019-05-29
(97) Date of publication of the European application 2021-04-14
(45) Date of publication and mention of the grant of the patent 2023-07-05
(46) Date of publication of the claims translation
PCT application
(86) Number PCT/US2019/034409
Date 2019-05-29
PCT application publication
(87) Number WO 2019/232060
Date 2019-12-05
Priority applications
(30) Number Date Country code
201862677419 P 2018-05-29 US
Inventors
(72)
EVULET, Andrei , US
Grantee
(73) Jetoptera, Inc. , 144 Railroad Avenue, Suite 100, Edmonds, WA 98020, US
Title
(54) STREAMLINE AIRFRAME WITH BOUNDARY INGESTION FLUIDIC PROPULSIVE ELEMENTS
  STREAMLINE AIRFRAME WITH BOUNDARY INGESTION FLUIDIC PROPULSIVE ELEMENTS